SBIR/STTR
Deployable Engine Air-Brake for Drag Management Applications, Phase I
Project Introduction
ATA Engineering, Inc, proposes an SBIR program to demonstrate an innovative engine air-brake (EAB) technology that uses a deployable swirl vane mechanism to switch the operation of a turbofan engine nozzle from a conventional to a "drag management" mode. Such "drag on demand" enables operational benefits such as slower, steeper, and/or aeroacoustically cleaner flight on approach, addressing NASA's need for active and passive control of aeroacoustic noise sources for conventional and advanced air
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Anticipated Benefits
The most immediate opportunity for this system is to assist NASA in the development of next generation quiet aircraft, including conventioanl tube and wing (current generation "N"+1), unconventional integrated airframe-propulsion system configurations (N+2), and advanced aircraft concepts (N+3). These aircraft are likely to have noise levels from the engine and airframe that are comparable. A deployable, quiet air-brake device will allow noise reduction by creating drag without the associated unsteady flow structures of devices such as flaps, slats, and undercarriage. In addition, these devices will enable steep approaches, thereby locating the noise source further from the affected communities. Finally, pairs of engine air-brakes operating in concert on multi-engine aircraft may be used for aircraft control and special maneuvering applications by performing, for example, an aircraft rudder function. An additional application for swirling exhaust flows is in the area of wake vortex Two complementary potential commercial markets exist for the proposed technology: (1) implementation in retrofit kits on older aircraft engines, and (2) implementation in future jet engines as an integral part of the design; i.e., modifying traditional engine exit guide vanes or bypass nozzles with a variable geometry mechanism that generates a swirling outflow in drag management mode. The first market has immediate potential (within 5 years), while the second market, although potentially much larger from a quantity standpoint, is a longer-term endeavor (likely 7 to 10 years to implementation). The retrofit market provides a simpler and faster opportunity to implement and demonstrate the technology before upselling it or its derivatives to the large engine Original Equipment Manufacturers. As part of this SBIR program, ATA will partner with small engine manufacturer Williams International to understand how the design may be incorporated into one or more of their engines. As the worl
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Primary U.S. Work Locations and Key Partners
| Organizations Performing Work | Role | Type | Location |
|---|---|---|---|
Langley Research Center
(LaRC)
|
Lead Organization | NASA Center | Hampton, Virginia |
| ATA Engineering, Inc. | Supporting Organization | Industry | San Diego, California |
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Organizational Responsibility
Responsible Mission Directorate:
- Space Technology Mission Directorate (STMD)
Lead Center / Facility:
- Langley Research Center (LaRC)
Responsible Program:
- SBIR/STTR
Project Management
Program Director:
Program Manager:
Principal Investigator:
- Parthiv Shah
Project Duration
Start: Feb 2012
End: Aug 2012
Technology Maturity (TRL)
| Start: | 3 |
| Current: | 3 |
| Estimated End: | 5 |
Applied Research
Development
Demo & Test
Technology Areas
Primary:
- TX01 Propulsion Systems
- TX01.3 Aero Propulsion
- TX01.3.1 Integrated Systems and Ancillary Technologies
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